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Acoustic Liner Program for future High-bypass-ratio Aircraft engines(Development of combustor)

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101C39 Subject Category: Aeronautical Technology PDF Responsible Representative: Kenichiro Nagai, Aeronautical Technology Directorate,Aviation Environmental Sustainability Innovation Contact Information: Naoyuki Okamura(okamura.naoyuki@jaxa.jp) Members: Taisuke Nambu, Hideji Saiki Abstract In this project, we will apply next-generation acoustic liner to combustor. To perform the numerical analysis of combustor with the acoustic liner by using HINOCA-AE which is CFD solver for aircraft engine combustors. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Development of a high-precision unstructured mesh flow solver for aerodynamic design of turbomachinery cascade

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101C13 Subject Category: Aeronautical Technology PDF Responsible Representative: ISHII Tatsuya, Director, Aviation Technology Directrate, Aviation Environmental Sustainability Innovation Hub Contact Information: Taisuke Nambu, Aviation Technology Directorate, Aviation Environmental Sustainability Innovation Hub(nambu.taisuke@jaxa.jp) Members: Manabu Hisida, Hamidreza Kheirandish, Junichi Kazawa, Takahisa Kohno, Taisuke Nambu, Kanako Yasue Abstract FaSTAR-Move-AE, a fluid analysis solver for unstructured meshes, which is mainly targeted at turbomachinery analysis, is developed. This solver will enable aerodynamic analysis of cascades・・・<<read more>>

Gas-Liquid Two Phase Flow Behavior Related to ECLSS

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23ECWU77 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Masato Sakurai, Manager for ECLSS Contact Information: Masato Sakurai(sakurai.masato@jaxa.jp) Members: Motoharu Kusano, Gaku Murakami, Masato Sakurai Abstract Elucidate the effects of gravity on gas-liquid two-phase flows to develop separation techniques for gas-liquid two-phase flows generated by the operation of the Environment Control and Life Support System (ECLSS). Reference URL N/A Reasons and benefits of using JAXA Supercomputer System In order・・・<<read more>>

Study on spacecraft dynamics

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23ECWU24 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Shujiro Sawai, Professor, Institute of Space and Astronautical Science Contact Information: Yusuke Maru(maru.yusuke@jaxa.jp) Members: Hiroto Aoyagi, Shoya Koshino, Ryota Miyajima, Kazuma Matsumoto, Yuma Miki, Daiki Watanabe, Maiko Yamakawa Abstract Numerical analysis on the dynamics of various spacecraft are peformed. Specifically, we will (1) design of the flow path shape of the air intake of an air breathing engine used in・・・<<read more>>

Study on future space transportation system - combined cycle engine (JAXA-Tohoku Univ. collaborative course)

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23ECWU07 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Sadatake Tomioka, Associate Principal Researcher, Research and Development Directorate, 4th Unit. Contact Information: Sadatake Tomioka (RInsertHereD directorate, 4th Research Unit)(tomioka.sadatake@jaxa.jp) Members: Sadatake Tomioka, Hironobu Nishiguchi, Ryota Ito Abstract Fully reusable launch vehicle will reduce the transportation cost and increase the space launch demands. Introduction of airbreathing engine will afford system weigth penalty necessary to realise reuablity by reducing on-board oxygen・・・<<read more>>